An attachment assembly a conically tapered missile body interface surface of a missile body attachment interface wedged against a conically tapered missile component interface surface of a missile body attachment interface. The missile body attachment interface also includes an engagement rod for locked engagement by a hook of the missile component attachment interface. Specifically, the missile component attachment interface includes an auto-adjusting assembly having a series of pivoting arms connected to a rotatable engagement drive at a first end thereof and a hook at a second end thereof. The auto-adjusting assembly is moveable between a first position and a second position, and between the second position and a third position. The missile component attachment interface includes a pre-loaded over-center mechanism operably coupled to the auto-adjusting assembly and configured to lock the hook in engagement with the engagement rod in the third position.

The invention relates to a method for reducing an imbalance of a projectile shell. The projectile shell has a body (1) which has a recess (4). By this recess (4), the body is provided with an inner wall (2) and an outer wall (3). In addition, a mouth hole (6) is provided, which is connected to the recess (4). A central axis (5) is now calculated from the outer geometrical shape of the projectile shell and a measurement is then performed to ascertain an imbalance of the projectile shell. On the basis of the measured imbalance, modified axis (8) is then calculated in relation to the central axis (5), and the body (1) is rotated about the modified axis (8) on the basis of the calculated modified axis (8). As the body (1) is rotated in this way, the projectile shell is machined to eliminate the imbalance as far as possible.

The invention relates to a method for reducing an imbalance of a projectile shell. The projectile shell has a body (1) which has a recess (4). By this recess (4), the body is provided with an inner wall (2) and an outer wall (3). In addition, a mouth hole (6) is provided, which is connected to the recess (4). A central axis (5) is now calculated from the outer geometrical shape of the projectile shell and a measurement is then performed to ascertain an imbalance of the projectile shell. On the basis of the measured imbalance, modified axis (8) is then calculated in relation to the central axis (5), and the body (1) is rotated about the modified axis (8) on the basis of the calculated modified axis (8). As the body (1) is rotated in this way, the projectile shell is machined to eliminate the imbalance as far as possible.

A safe and reliable multi-component projectile enables cost effective manufacturing and assembly of the projectile. Major components of the projectile are joined by a plurality of shear pins interfacing with scalloped geometry of the components. The components are then held together by forcibly joining them using a hybrid annular-cantilevered snap fit joint. The tooth and groove arrangement exists where the teeth are at the end of a spring-leaf like feature of one of the mating parts and the groove is located on the opposite mating part.

A safe and reliable multi-component projectile enables cost effective manufacturing and assembly of the projectile. Major components of the projectile are joined by a plurality of shear pins interfacing with scalloped geometry of the components. The components are then held together by forcibly joining them using a hybrid annular-cantilevered snap fit joint. The tooth and groove arrangement exists where the teeth are at the end of a spring-leaf like feature of one of the mating parts and the groove is located on the opposite mating part.

According to a first aspect of the present invention, there is provided a reconnaissance and communication assembly, adapted to be launched from a gun barrel into the air. The assembly comprises a carrier (with a cavity) and a payload (within the cavity). The payload is arranged to be controllably expelled from the carrier and once expelled from the carrier, the payload transmits a signal.

According to a first aspect of the invention, there is provided a programmable system for a munition, comprising: an electroacoustic transducer, arranged to receive an acoustic signal comprising data, and convert that signal into an electrical signal comprising data; a processor, arranged to receive and process the electrical signal comprising data, and to use that data in programming of the programmable system.

According to a first aspect of the invention, there is provided an object for moving through a fluid, the object comprising: an outer housing, arranged to be exposed to a hydrostatic pressure exerted by the fluid; a strain gauge, arranged to obtain an indication of the hydrostatic pressure, wherein a first part of the strain gauge is arranged to be in contact with the outer housing, such that the strain gauge is arranged to obtain an indication of the hydrostatic pressure by obtaining an indication of the strain on the housing.

An attachment assembly includes a conically tapered missile body interface surface of a missile body attachment interface wedged against a conically tapered missile component interface surface of a missile body attachment interface. The missile body attachment interface also includes an engagement rod for locked engagement by a hook of the missile component attachment interface. Specifically, the missile component attachment interface includes an auto-adjusting assembly having a series of pivoting arms connected to a rotatable engagement drive at a first end thereof and a hook at a second end thereof. The auto-adjusting assembly is moveable between a first position and a second position, and between the second position and a third position. The missile component attachment interface includes a pre-loaded over-center mechanism operably coupled to the auto-adjusting assembly and configured to lock the hook in engagement with the engagement rod in the third position.

An attachment assembly includes a conically tapered missile body interface surface of a missile body attachment interface wedged against a conically tapered missile component interface surface of a missile body attachment interface. The missile body attachment interface also includes an engagement rod for locked engagement by a hook of the missile component attachment interface. Specifically, the missile component attachment interface includes an auto-adjusting assembly having a series of pivoting arms connected to a rotatable engagement drive at a first end thereof and a hook at a second end thereof. The auto-adjusting assembly is moveable between a first position and a second position, and between the second position and a third position. The missile component attachment interface includes a pre-loaded over-center mechanism operably coupled to the auto-adjusting assembly and configured to lock the hook in engagement with the engagement rod in the third position.